The effects of Reynolds number, rotor incidence angle, and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage
By: reported by M.F. Blair, O.L. Anderson.
Contributors: Anderson, Olof L.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA/CR-183891.
Publisher: United Technologies Research Center; National Aeronautics and Space Administration
Published: 1989
Place of publication: East Hartford, Conn; [Washington, D.C
Language: eng
Format: Microform
Subjects: Heat transfer.; High pressure.; Navier-Stokes equation.; Reynolds number.; Rotors.; Space shuttle main engine.; Surface roughness.; Temperature distribution.; Turbine pumps.
Notes: Shipping list no.: 91-0122-M.

"Date: November 1989."

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/18/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900014415%5F1990014415.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 2 microfiches.